Application of the Restricted Hyperbolic Three-Body Problem to a Sun-Star-Comet System

Details Application of the Restricted Hyperbolic Three-Body Problem to a Sun-Star-Comet System Application of the Restricted Hyperbolic Three-Body Problem to a Sun-Star-Comet System

Aug 1972

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1972cemec...6...22f&link_type=abstract

Celestial Mechanics, Volume 6, Issue 1, pp.22-26

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1

Scientific paper

The equations of motion for a third body of small mass are developed in
the problem where the two primary bodies are in hyperbolic orbits about
each other. The equations are applied to a hypothetical star-sun-comet
system to determine the effect of the stellar encounter on the orbit of
the comet.

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